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You searched for: subject:"Aerodynamics--Research."
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[texts]Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854698&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research
Downloads: 86
[texts]Effect of powered propellers on the aerodynamic characteristics and the porpoising stability of a dynamic model of a long-range flying boat - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805116&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 85
[texts]Wind-tunnel investigation of the aerodynamic and structural deflection characteristics of the Goodyear inflatoplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003833712&ix=nu&I=0&V=D&pm=1
Keywords: Research aircraft; Aerodynamics--Research
Downloads: 118
[texts]Some measurements of time and space correlation in wind tunnel - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807829&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence--Research; Aerodynamics--Research
Downloads: 105
[texts]Experimental verification of the rudder-free stability theory for an airplane model equipped with rudders having negative floating tendency and negligible friction - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806635&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 123
[texts]Flight investigation of internally balanced sealed ailerons in the presence of a balanced split flap - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805102&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 97
[texts]Force tests of a 1/5-scale model of the type GB-5 controllable glide bomb - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003610203&ix=nu&I=0&V=D&pm=1
Keywords: Guided bombs; Aerodynamics--Research
Downloads: 122
[texts]Column and plate compressive strengths of aircraft structural materials extruded 75S-T aluminum-alloy - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807482&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Testing; Aerodynamics--Research
Downloads: 117
[texts]Effect of initial displacement of the center support on the buckling of a column continuous over three supports - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804949&ix=nu&I=0&V=D&pm=1
Keywords: Buckling (Mechanics; Aerodynamics--Research
Downloads: 121
[texts]NACA impact basin and water landing tests of a float model at various velocities and weights - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804832&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 128
[texts]Effects of compressibility on the maximum lift characteristics and spanwise load distribution of a 12-foot-span fighter-type wing of NACA 230-series airfoil sections - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614876&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Compressibility; Aerodynamics--Research
Downloads: 111
[texts]Approximate determination of the power required to move control surfaces as related to control-booster design - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614183&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 99
[texts]Apparatus for measurements of time and space correlation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807826&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence--Research; Aerodynamics--Research
Downloads: 90
[texts]Effect of compressibility on the hovering performance of two 10-foot-diameter helicopter rotors tested in the Langley full-scale tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834396&ix=nu&I=0&V=D&pm=1
Keywords: Rotors (Helicopters; Aerodynamics--Research
Downloads: 110
[texts]Wind-tunnel tests of dual-rotating propellers with systematic differences in number of blades, blade setting, and rotational speed of front and rear propellers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638089&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 121
[texts]Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808495&ix=nu&I=0&V=D&pm=1
Keywords: Afterburners--Research; Aerodynamics--Research
Downloads: 74
[texts]Simple method for estimating terminal velocity including effect of compressibility on drag - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638273&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 94
[texts]Theoretical and experimental dynamic loads for a prismatic float having an angle of dead rise of 22 1/2° - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638573&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes--Hydrodynamics; Aerodynamics--Research
Downloads: 93
[texts]Effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614166&ix=nu&I=0&V=D&pm=1
Keywords: Yawing (Aerodynamics; Aerodynamics--Research
Downloads: 187
[texts]Aerodynamic tests of an M-31 bomb in the 8-foot high-speed tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003612647&ix=nu&I=0&V=D&pm=1
Keywords: Projectiles, Aerial; Aerodynamics--Research
Downloads: 73
[texts]Effect on stability and control of a pusher propeller behind conventional tail surfaces as determined by tests of a powered model in the free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805344&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 167
[texts]Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834476&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 85
[texts]Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics--Research; Drag (Aerodynamics
Downloads: 185
[texts]On slender-body theory at transonic speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808938&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics, Transonic; Aerodynamics--Research
Downloads: 264
[texts]Analysis of available data on the effectiveness of ailerons without exposed overhang balance - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807486&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 133
[texts]Recovery corrections for butt-welded, straight-wire thermocouples in high-velocity, high-temperature gas streams - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810742&ix=nu&I=0&V=D&pm=1
Keywords: Thermocouples; Aerodynamics--Research
Downloads: 103
[texts]Frequency of occurrence of atmospheric gusts and of related loads on airplane structures - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808565&ix=nu&I=0&V=D&pm=1
Keywords: Airframes; Aerodynamics--Research
Downloads: 88
[texts]Effects of heat-capacity lag in gas dynamics - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614317&ix=nu&I=0&V=D&pm=1
Keywords: Carbon dioxide; Aerodynamics--Research
Downloads: 110
[texts]Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616150&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 116
[texts]Resistance tests of models of three flying-boat hulls with a length-beam ration of 10.5 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638098&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Nacelles; Aerodynamics--Research
Downloads: 123
[texts]Review of the physical and thermodynamic properties of boric oxide - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853251&ix=nu&I=0&V=D&pm=1
Keywords: Thermodynamics--Research; Aerodynamics--Research
Downloads: 71
[texts]Climb and high-speed tests of a Curtiss no. 714-1C2-12 four-blade propeller on the Republic P-47C airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807441&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 122
[texts]Influence of vertical-tail design and direction of propeller rotation on trim characteristics of a twin-engine-airplane model with one engine inoperative - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804754&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Testing; Aerodynamics--Research
Downloads: 183
[texts]Effects on low-speed spray characteristics of various modifications to a powered model of the Boeing XPBB-1 flying boat - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804846&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 100
[texts]Theory of propellers.:I, Determination of the circulation function and the mass coefficient for dual-rotating propellers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003622107&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 140
[texts]Langley full-scale tunnel investigation of the factors affecting the directional stability and trim characteristics of a fighter-type airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614294&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Aerodynamics--Research
Downloads: 141
[texts]Electromagnetic-analogy method of solving lifting-surface-theory problems - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613188&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 130
[texts]Theory of propellers.: III, the slipstream contraction with numerical values for two-blade and four-blade propellers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638511&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 186
[texts]On the gas dynamics of a rotating impeller - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807542&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 91
[texts]Some notes on the determination of the stick-free neutral point from wind-tunnel data - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804989&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 106
[texts]Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807484&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 110
[texts]Effect of bluntness on the drag of spherical-tipped truncated cones of fineness ratio 3 at Mach numbers 1.2 to 7.4 - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810613&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Aerodynamics--Research
Downloads: 213
[texts]Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834456&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 140
[texts]Flight investigation of boundary-layer and profile-drag characteristics of smooth wing sections of a P-47D airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613546&ix=nu&I=0&V=D&pm=1
Keywords: Bombers; Compressibility; Aerodynamics--Research
Downloads: 83
[texts]Measurements of aerodynamic heat transfer and boundary-layer transition on a 10° cone in free flight at supersonic Mach numbers up to 5.9 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854699&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research
Downloads: 64
[texts]Effect of fabric deflection at high speeds on the aerodynamic characteristics of the horizontal tail surface of an SB2D-1 airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804830&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 132
[texts]Comparison of tail and wing-tip spin-recovery parachutes as determined by tests in the Langley 20-foot free-spinning tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616345&ix=nu&I=0&V=D&pm=1
Keywords: Parachutes; Aerodynamics--Research
Downloads: 164
[texts]Column and plate compressive strengths of aircraft structural materials 24S-T aluminum-alloy sheet - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804757&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Testing; Aerodynamics--Research
Downloads: 143
[texts]Flight investigation of NACA aileron modifications for the improvement of the lateral control characterisitcs of a high-speed fighter airplance - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804734&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Aerodynamics--Research
Downloads: 128
[texts]Theories of turbulence - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807732&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence; Aerodynamics--Research
Downloads: 159
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